Target tracking in maneuver centered coordinates

J. A. Roecker, C. McGillem
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引用次数: 3

Abstract

Aircraft targets normally maneuver on circular paths which has led to tracking filters based on circular turns. The authors introduce a new coordinate system to track circular maneuvers with a simple Kalman filter. When the maneuver is detected the tracker switches to a polar coordinate system located at the center of the maneuver. The state vector will then have radius, angle, and angular velocity as its components. This makes the process equation linear, allowing a simple Kalman filter to be used throughout the turn. The center of maneuver is estimated with each new measurement to adjust for possible changes. This investigation also examines maneuver detection methods and how they apply to the circular tracking problem. The method is then compared to the methods of Y. Bar-Shalom and K. Birmiwal (1982) and P.L. Bogler (1987) on various circular paths. The resulting algorithm displays improved performance over methods based on constant x-y accelerations when tracing circular turns.<>
以机动中心坐标跟踪目标
飞机目标通常在圆形路径上机动,这导致了基于圆形转弯的跟踪滤波器。作者介绍了一种新的坐标系统,用一个简单的卡尔曼滤波来跟踪圆机动。当检测到机动时,跟踪器切换到位于机动中心的极坐标系。状态向量将有半径、角度和角速度作为其分量。这使得过程方程线性,允许在整个转弯中使用简单的卡尔曼滤波器。机动中心估计与每一个新的测量,以调整可能的变化。本研究还考察了机动检测方法以及它们如何应用于圆形跟踪问题。然后将该方法与Y. Bar-Shalom和K. Birmiwal(1982)以及P.L. Bogler(1987)在各种圆形路径上的方法进行比较。所得到的算法在跟踪圆形转弯时,比基于恒定x-y加速度的方法显示出更好的性能
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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